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1.发明公开SYSTEME D'ACTIONNEMENT POUR UN PANNEAU MOBILE D'UNE NACELLE DE TURBOREACTEUR 审中-公开宝贝系列FÜREINE BEWEGLICHE平底锅EINER GONDEL EINES TURBOJETS
公开(公告)号：EP2419330A1
公开(公告)日：2012-02-22
申请号：EP10723216.7
申请日：2010-04-07
申请人： Aircelle , Sagem Défense Sécurité
摘要： The invention relates to a system for actuating a plurality of actuators (15) that can move a mobile panel of an aircraft nacelle. Said system comprises at least two motors (16) that can drive the actuators (15), the two motors (16) being controlled and supplied by at least two separate control units (33, 35), and the actuators (15) being mechanically interconnected by a mechanical transmission (37). The invention also relates to a nacelle comprising such an actuating system.
摘要翻译： 本发明涉及一种用于致动能够移动飞机机舱的移动面板的多个致动器（15）的系统。 所述系统包括至少两个可驱动致动器（15）的马达（16），两个马达（16）由至少两个单独的控制单元（33,35）控制和供应，并且致动器（15）机械地 通过机械传动装置互连（37）。 本发明还涉及包括这种致动系统的机舱。
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公开(公告)号：EP2440453A1
公开(公告)日：2012-04-18
申请号：EP10725122.5
申请日：2010-06-10
发明人： RODRIGUES, Fernand
摘要： The invention relates to a device (4) for actuating a control surface (2) of an aircraft, comprising: - a frame intended to be mounted fixed in relation to a structure of an aircraft, - a bell crank part (7) mobile in rotation in relation to the frame around an axis of rotation (X, X') and adapted in order to be connected to a mechanical unit (1) for displacement of the control surface (2), - a slider (6) intended to be connected to a drive member (5), the slider (6) being mobile in translation in relation to the frame according to a direction of translation, parallel to the axis of rotation (X, X') of the bell crank part (7), - first connecting means (61) between the slider (6) and the bell crank part (7) in order to convert a displacement in translation of the slider (6) generated by the drive member (5) into a displacement in rotation of the bell crank part (7), in order to actuate the mechanical unit (1) for displacement of the control surface (2),an input part (53, 16) able to be driven in rotation by the motor, - a control rod mounted fixed in relation to the frame and extending parallel to the axis of rotation (X) of the input part and at a distance from the latter, in order to block in rotation the slider in relation to the frame and authorize a translation of the slider in relation to the frame, the control rod extends through the slider (6). Application specific to the actuating of control surfaces incorporated into a thin airfoil.
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公开(公告)号：EP2630357A1
公开(公告)日：2013-08-28
申请号：EP11784610.5
申请日：2011-10-21
发明人： RODRIGUES, Fernand
CPC分类号： F02C7/36 , F02K1/72 , F02K1/763 , F05D2260/40311
摘要： The invention relates to an actuation system (100) for a propulsive unit including a nacelle, a turbojet engine, and an air circulation channel defined between the nacelle and the turbojet engine, the actuation system (100) including: a body and a connection device for attaching the body to the nacelle, the connection device enabling the body to move relative to the nacelle along two axes of rotation; a first member for moving a flap for controlling the airflow in the channel, the first member extending from the body and having a first point for attaching the first member to the flap; a second member for moving a thrust-reversing flap, the second member extending from the body and having a second point for attaching the second member to the flap, the body being arranged between the first and second attachment points; and a transmission device (40) having an input (42), a first output (44) connected to the first member (50), and a second output (43) connected to the second member (70), the transmission device (40) being capable of selectively transmitting input movement towards the first output, in order to move the flow-controlling flap, or towards the second output, in order to move the thrust-reversing flap.
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公开(公告)号：EP2630357B1
公开(公告)日：2015-07-15
申请号：EP11784610.5
申请日：2011-10-21
发明人： RODRIGUES, Fernand
CPC分类号： F02C7/36 , F02K1/72 , F02K1/763 , F05D2260/40311
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